JPS4949012A - - Google Patents
Info
- Publication number
- JPS4949012A JPS4949012A JP48065291A JP6529173A JPS4949012A JP S4949012 A JPS4949012 A JP S4949012A JP 48065291 A JP48065291 A JP 48065291A JP 6529173 A JP6529173 A JP 6529173A JP S4949012 A JPS4949012 A JP S4949012A
- Authority
- JP
- Japan
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2715472A GB1424197A (en) | 1972-06-09 | 1972-06-09 | Combustion chambers for gas turbine engines |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS4949012A true JPS4949012A (US06373033-20020416-M00071.png) | 1974-05-13 |
| JPS5411844B2 JPS5411844B2 (US06373033-20020416-M00071.png) | 1979-05-18 |
Family
ID=10255088
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6529173A Expired JPS5411844B2 (US06373033-20020416-M00071.png) | 1972-06-09 | 1973-06-09 |
Country Status (6)
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5381657U (US06373033-20020416-M00071.png) * | 1976-12-09 | 1978-07-06 | ||
| JPH0387059U (US06373033-20020416-M00071.png) * | 1989-12-11 | 1991-09-04 | ||
| JP2004507700A (ja) * | 2000-05-01 | 2004-03-11 | エリオット・エナジー・システムズ・インコーポレイテッド | エネルギーシステムと併用する環状燃焼器 |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1552132A (en) * | 1975-11-29 | 1979-09-12 | Rolls Royce | Combustion chambers for gas turbine engines |
| GB1571213A (en) * | 1977-01-28 | 1980-07-09 | Kainov G | Combustion chamber for gas turbine engine |
| DE2723546A1 (de) * | 1977-05-25 | 1978-11-30 | Motoren Turbinen Union | Brennkammer, insbesondere ringumkehrbrennkammer fuer gasturbinentriebwerke |
| DE2728399C2 (de) * | 1977-06-24 | 1982-04-22 | Brown, Boveri & Cie Ag, 6800 Mannheim | Brennkammer für eine Gasturbine |
| US4195476A (en) * | 1978-04-27 | 1980-04-01 | General Motors Corporation | Combustor construction |
| US4361010A (en) * | 1980-04-02 | 1982-11-30 | United Technologies Corporation | Combustor liner construction |
| US4765136A (en) * | 1985-11-25 | 1988-08-23 | United Technologies Corporation | Gas turbine engine augmentor |
| US4928479A (en) * | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
| US4944152A (en) * | 1988-10-11 | 1990-07-31 | Sundstrand Corporation | Augmented turbine combustor cooling |
| US4949545A (en) * | 1988-12-12 | 1990-08-21 | Sundstrand Corporation | Turbine wheel and nozzle cooling |
| US5109671A (en) * | 1989-12-05 | 1992-05-05 | Allied-Signal Inc. | Combustion apparatus and method for a turbine engine |
| US5069033A (en) * | 1989-12-21 | 1991-12-03 | Sundstrand Corporation | Radial inflow combustor |
| US5113647A (en) * | 1989-12-22 | 1992-05-19 | Sundstrand Corporation | Gas turbine annular combustor |
| US5165226A (en) * | 1991-08-09 | 1992-11-24 | Pratt & Whitney Canada, Inc. | Single vortex combustor arrangement |
| US5237813A (en) * | 1992-08-21 | 1993-08-24 | Allied-Signal Inc. | Annular combustor with outer transition liner cooling |
| US5271220A (en) * | 1992-10-16 | 1993-12-21 | Sundstrand Corporation | Combustor heat shield for a turbine containment ring |
| US5746048A (en) * | 1994-09-16 | 1998-05-05 | Sundstrand Corporation | Combustor for a gas turbine engine |
| US5628193A (en) * | 1994-09-16 | 1997-05-13 | Alliedsignal Inc. | Combustor-to-turbine transition assembly |
| US6079199A (en) * | 1998-06-03 | 2000-06-27 | Pratt & Whitney Canada Inc. | Double pass air impingement and air film cooling for gas turbine combustor walls |
| US6405703B1 (en) | 2001-06-29 | 2002-06-18 | Brian Sowards | Internal combustion engine |
| US6925810B2 (en) * | 2002-11-08 | 2005-08-09 | Honeywell International, Inc. | Gas turbine engine transition liner assembly and repair |
| US7308794B2 (en) * | 2004-08-27 | 2007-12-18 | Pratt & Whitney Canada Corp. | Combustor and method of improving manufacturing accuracy thereof |
| DE102005008421A1 (de) * | 2005-02-24 | 2006-08-31 | Alstom Technology Ltd. | Verfahren zum Verbrennen eines Brennstoffs und zugehörige Brennkammer |
| JP2008536333A (ja) * | 2005-04-13 | 2008-09-04 | コーニング インコーポレイテッド | 同調可能外部キャビティレーザのためのモード整合システム |
| US7954326B2 (en) * | 2007-11-28 | 2011-06-07 | Honeywell International Inc. | Systems and methods for cooling gas turbine engine transition liners |
| US8640464B2 (en) * | 2009-02-23 | 2014-02-04 | Williams International Co., L.L.C. | Combustion system |
| US8864492B2 (en) * | 2011-06-23 | 2014-10-21 | United Technologies Corporation | Reverse flow combustor duct attachment |
| US9879862B2 (en) | 2013-03-08 | 2018-01-30 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine afterburner |
| US20150323185A1 (en) | 2014-05-07 | 2015-11-12 | General Electric Compamy | Turbine engine and method of assembling thereof |
| US11674445B2 (en) * | 2021-08-30 | 2023-06-13 | Collins Engine Nozzles, Inc. | Cooling for continuous ignition devices |
| US11674446B2 (en) * | 2021-08-30 | 2023-06-13 | Collins Engine Nozzles, Inc. | Cooling for surface ignitors in torch ignition devices |
| US20230296250A1 (en) * | 2022-03-21 | 2023-09-21 | General Electric Company | Turbine engine combustor and combustor liner |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2531810A (en) * | 1946-06-05 | 1950-11-28 | Kellogg M W Co | Air inlet arrangement for combustion chamber flame tubes |
| BE507258A (US06373033-20020416-M00071.png) * | 1950-12-02 | |||
| US3333414A (en) * | 1965-10-13 | 1967-08-01 | United Aircraft Canada | Aerodynamic-flow reverser and smoother |
| GB1289523A (US06373033-20020416-M00071.png) * | 1969-03-17 | 1972-09-20 | ||
| US3613360A (en) * | 1969-10-30 | 1971-10-19 | Garrett Corp | Combustion chamber construction |
| US3653207A (en) * | 1970-07-08 | 1972-04-04 | Gen Electric | High fuel injection density combustion chamber for a gas turbine engine |
| US3671171A (en) * | 1970-11-27 | 1972-06-20 | Avco Corp | Annular combustors |
-
1972
- 1972-06-09 GB GB2715472A patent/GB1424197A/en not_active Expired
-
1973
- 1973-06-07 IT IT50516/73A patent/IT989653B/it active
- 1973-06-08 DE DE2329367A patent/DE2329367C2/de not_active Expired
- 1973-06-09 JP JP6529173A patent/JPS5411844B2/ja not_active Expired
- 1973-06-11 US US368576A patent/US3869864A/en not_active Expired - Lifetime
- 1973-06-12 FR FR7321313A patent/FR2188055B1/fr not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5381657U (US06373033-20020416-M00071.png) * | 1976-12-09 | 1978-07-06 | ||
| JPS5638389Y2 (US06373033-20020416-M00071.png) * | 1976-12-09 | 1981-09-08 | ||
| JPH0387059U (US06373033-20020416-M00071.png) * | 1989-12-11 | 1991-09-04 | ||
| JP2004507700A (ja) * | 2000-05-01 | 2004-03-11 | エリオット・エナジー・システムズ・インコーポレイテッド | エネルギーシステムと併用する環状燃焼器 |
| JP4851674B2 (ja) * | 2000-05-01 | 2012-01-11 | キャプストーン タービン コーポレーション | エネルギーシステムと併用する環状燃焼器 |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1424197A (en) | 1976-02-11 |
| JPS5411844B2 (US06373033-20020416-M00071.png) | 1979-05-18 |
| FR2188055B1 (US06373033-20020416-M00071.png) | 1976-09-17 |
| US3869864A (en) | 1975-03-11 |
| DE2329367C2 (de) | 1981-12-24 |
| FR2188055A1 (US06373033-20020416-M00071.png) | 1974-01-18 |
| IT989653B (it) | 1975-06-10 |
| DE2329367A1 (de) | 1973-12-20 |
